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VELOX-P2 [TU München]

VELOX-P is a 1U CubeSat mission by Nanyang Technological University, Singapore, to develop and orbit a CubeSat for technology demonstration, to test in-house attitude determination and control system, power subsystem, and to support a dual-FOV sun sensor payload. The Cubesat VELOX Pwill be launched into experimental high inclination circular orbit at 300 km on an Interorbital Neptune flight from off-shore California with a number of other spacecraft. For its 8-12 weeks in orbit, VELOX Pwill log telemetry data from its various subsystems and send them down to our mission control center for analysis. As the Neptune launch vehicle is much delayed, a launch date can not be estimated.

VELOX-P2 is also 1U cubesat mission for technology demonstration to test in house ADAC system, power sub-system and to support a dual FOV suns sensor payload.

Nation: Singapore
Type / Application: Technology
Operator: Nanyang Technological University, Singapore
Contractors: Nanyang Technological University, Singapore
Configuration: CubeSat (1U)
Propulsion: None
Power: Solar cells, batteries
Mass: 1 kg
Orbit: 593 km × 699 km, 97.80° (#2)
Satellite COSPAR Date LS Launch Vehicle Remarks
VELOX-P - Neptune with ?
VELOX P2 2013-066Y 21.11.2013 Do LC-370/13 Dnepr with DubaiSat 2, STSAT 3, WNISAT 1, SkySat 1, BRITE-PL, AprizeSat 7, AprizeSat 8, UniSat 5, Delfi-n3Xt, Dove 3, Dove 4, Triton 1, CINEMA 2, CINEMA 3, CubeBug 2, GOMX 1, NEE 02 Krysaor, FUNcube 1, HiNCube, ZACUBE 1, ICube 1, HumSat-D, PUCP-SAT 1, First-MOVE, UWE 3, Pocket-PUCP, QubeScout S1, Wren